As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 339.723 WAS FOUND CRACKED (0.703"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-019 & EO ATI-070505. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.